N372NW

Service difficulty reports · 143

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N372NW' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DALA2022042903024None · noneSHIP 3272 -ATO- AT 60KTS DUE TO HOT BRAKE ECAM MSG. CORRECTIVE ACTION: REPLACED #1 BRAKE ASSEMBLY AND #1 BRAKE TEMP SENSOR. OK FOR SERVICE. (8664668)Apr 28, 2022 · N372NW · Airbus A320212 · Landing Gear Brake SystemSDR DALA2021080504444Skin · corrodedSHIP 3272 CORROSION COMMON TO UPPER SKIN PANEL OF LH WING. CORRECTIVE ACTION: COMPLIED WITH ERA 589793-14AD REV ORIG. CONTINUE ON MONITOR INSPECTION. (1899788)Aug 4, 2021 · N372NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2021080504443Skin · corrodedSHIP 3272 CORROSION COMMON TO UPPER SKIN PANEL OF LH WING. CORRECTIVE ACTION: COMPLIED WITH ERA 589793-14AD REV ORIG. CONTINUE ON MONITOR INSPECTION. (1899787)Aug 4, 2021 · N372NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2021080504442Skin · corrodedSHIP 3272 CORROSION COMMON TO UPPER SKIN PANEL OF LH WING. CORRECTIVE ACTION: COMPLIED WITH ERA 589793-14AD REV ORIG. CONTINUE ON MONITOR INSPECTION. (1899784)Aug 4, 2021 · N372NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2021042602398Panel · no testSHIP 3272 DURING TEST FOUND SEAT 26 ABC PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7588359)Apr 24, 2021 · N372NW · Airbus A320212 · Emergency EquipmentSDR DALA2021042602397Panel · no testSHIP 3272 DURING TEST FOUND SEAT 23 DEF PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7588358)Apr 24, 2021 · N372NW · Airbus A320212 · Emergency EquipmentSDR DALA2021021000772Skin · corrodedSHIP 3272 CORROSION UPPER SURFACE TRAILING EDGE AT LEVEL OF RIB 10 ON LH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER ER/A 589793-14AD RE.ORIGINAL AND PRI 589793-14 REV 0, 1 AND 2. (1726613)Feb 9, 2021 · N372NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2021021000773Skin · corrodedSHIP 3272 TWO SPOTS OF CORROSION FOUND ON TOP SKIN PANEL 2, LWR SURFACE TE OVERHANG AT RIBS 9-12 - LHS WING. CORRECTIVE ACTION: COMPLIED WITH 589793-14. CONT ON MON INSP. (1726109)Feb 8, 2021 · N372NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2021020400670Floor Panel · crackedSHIP 3272 CRACK INDICATION ON FR36 LT PRESSURE FLOOR PANEL FASTENER HOLE A AT Y 1292.0. CORRECTIVE ACTION PERFORMED REPAIR PER DELTA WORK CARD AMDS 5311-01171-04A.Feb 3, 2021 · N372NW · Airbus A320212 · Fuselage Floor PanelSDR DALA2021020100599Frame · crackedSHIP 3272 CRACK FRAME 36 THAT DOES NOT EXCEED THE AUTHORIZED REPAIR AREA WAS FOUND AT THE PRESSURE PLATE AREA BETWEEN FR 35LT AND FR 36LT. CORRECTIVE ACTION: MODIFIED FRAME PER DELTA WORK CARD 5311-01171-04A, AA 5311-01171, SB A320-53-1263, AD-2018-06-04.Jan 31, 2021 · N372NW · Airbus A320212 · Fuselage Main, FrameSDR DALA2021020100590Skin · corrodedSHIP 3272 CORROSION UPPER SURFACE LOCATED AT TRAILING EDGE AREA AND AT LEVEL OF RIB 10 ON RT WING. CORRECTIVE ACTION EVALUATED REWORKED AREA PER A320 SRM 57-21-11-283-013.Jan 30, 2021 · N372NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2021020100586Skin · corrodedSHIP 3272 CORROSION UPPER SURFACE TRAILING EDGE AT LEVEL OF RIB 9 ON LT WING. EVALUATED REWORKED AREA PER A320 SRM 57-21-11-283-013.Jan 29, 2021 · N372NW · Airbus A320212 · Wing, Plate/SkinSDR DALA2021012900555Flap · corrodedCORROSION UPPER SURFACE LOCATED AT TRAILING EDGE AREA AND BETWEEN RIB 12 T O RIB 13 ON RT WING. CORRECTIVE ACTION: REMOVED CORROSION, PER A320 SRM 57-21-11-283-013.Jan 29, 2021 · N372NW · Airbus A320212 · Trailing Edge FlapsSDR DALA2021012900554Flap · corrodedCORROSION UPPER SURFACE TRAILING EDGE AREA BETWEEN RIB 12 AND RIB 13 ON LT WING. CORRECTIVE ACTION: REWORKED CORROSION, PER SRM A320 57-21-11-283-013.Jan 29, 2021 · N372NW · Airbus A320212 · Leading Edge DevicesSDR DALA2021012900553Flap · corrodedCORROSION UPPER SURFACE LOCATED AT TRAILING EDGE AREA AND AT LEVEL OF RIB 17 ON RT WING. CORRECTIVE ACTION: REWORKED AREA, PER A320 SRM 57-21-11-283-013.Jan 29, 2021 · N372NW · Airbus A320212 · Trailing Edge FlapsSDR DALA2019121097213Window Post · crackedDURING HFEC INSPECTION OF R/H FLIGHT DECK WINDOW ALI FOUND EVIDENCE OF A CRACK ON LOWER ATTACHMENT SIDE POST, REPAIR PER ERA 583733-14AD REV ODec 7, 2019 · N372NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2019101425875Cover · missingEMERGENCY LIGHT 14D MISSING COVER, LIGHT OPERATES NORMALLY, REPLACED COVEROct 12, 2019 · N372NW · Airbus A320212 · Emergency LightingSDR DALA2019101805983Lens · missingSEAT 14D EMERGENCY ESCAPE PATH LIGHT MISSING COVER LIGHT OPERATES NORMALLY, REMOVED & INSTALLED SERVICEABLE REPLACEMENT SEAT 14D EMERGENCY PATH LIGHT ASSYOct 11, 2019 · N372NW · Airbus A320212 · Emergency LightingSDR DALA2019092105476Light · brokenEMERGENCY FLOOR LIGHTING 14D BROKE OFF SEAT, RESECURED LIGHT ASSY AT 14D.Sep 20, 2019 · N372NW · Airbus A320212 · Emergency LightingSDR DALA2019062513847Battery Pack · no testEPSU BATTERY EMER R 33-51-38 DISPLAYED ON CIDS EPSU SELF-TEST, REPLACED EPSU 12WL BATTERYJun 21, 2019 · N372NW · Airbus A320212 · Emergency LightingSDR DALA2018100905997Door Frame · crackedCRACK INDICATION ON PASSENGER CREW DOOR FRAME 16 DOUBLE JOGGLE AREA FASTENER HOLE LOCATED 4.5 IN ABOVE DOOR STOP NR 7 AND .5 IN. FROM DOOR CUTOUT EDGE, RIGHT HAND SIDE IN PASSENGER CABIN. PERFORMED TIME LIMITED REPAIR IAW PRI/ERA 571448-14-AD.Oct 8, 2018 · N372NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2018100905999Epsu · not reportedEPSU CENTER POSITION IN PASSENGER CABIN. REPLACED EMERGENCY POWER SUPPLY UNIT. OPERATION CHECKS GOOD.Oct 7, 2018 · N372NW · Airbus A320212 · Emergency LightingSDR DALA2018100805934Fitting · crackedCRACK INDICATION ON FRAME 16 IN OPEN INBOARD UPPER HOLE AT DOOR STOP NR 7 RIGHT HAND SIDE AT FORWARD GALLEY AREA. REPLACED INTERCOSTAL FITTING LOCATED AT LEVEL STOP FITTING NR 7 BETWEEN FR 15 TO FR16 RIGHT HAND SIDE IAW SRM 51-72-11 AND DWG R5311-3020.Oct 7, 2018 · N372NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018100505933Floorbeam · corrodedCORROSION FLOORBEAM +Y1292 FRAME 66 TO FRAME 68 AT AFT GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D53472001.Oct 4, 2018 · N372NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018100405932Door Sill · corrodedCORROSION LOWER SILL AT AFT GALLEY AREA FRAME 66 TO FRAME 68 STRINGER 23L. REPLACED IAW SRM 51-72-11 AND DWG D53480505.Oct 4, 2018 · N372NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018100405931Dummy Rail · corrodedCORROSION RAIL DUMMY Y503.2 LOCATED FRAME 12 TO FRAME 16 AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D5311282.Oct 4, 2018 · N372NW · Airbus A320212 · Fuselage, Seat/Cargo Attach FittingsSDR DALA2018100305886Skin · dentedDENT SKIN LOCATED BETWEEN FRAME 79 TO FRAME 80 STRINGER 1 TO STRINGER 3 LEFT HAND UPPER ON TAIL. PERMANENT REPAIR PERFORMED IAW SRM 53-51-11-300-002..Oct 2, 2018 · N372NW · Airbus A320212 · Fuselage Main, Plate/SkinSDR DALA2018100205884Floorbeam · corrodedCORROSION FLOORBEAM +Y765 LOCATED FROM FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D53112812.Oct 1, 2018 · N372NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018100105883Floorbeam · corrodedCORROSION FLOORBEAM -Y162.5 FRAME 68 TO FRAME 69 AT AFT GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D53472001.Sep 30, 2018 · N372NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018100105882Door Sill · corrodedCORROSION LOWER SILL AT AFT GALLEY AREA FRAME 66 TO FRAME 68 STRINGER 23R. REPLACED IAW SRM 51-72-11 AND DWG D53480505.Sep 30, 2018 · N372NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018100105881Floorbeam · corrodedCORROSION FLOORBEAM -Y1292 FRAME 66 TO FRAME68 AT AFT GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D53472816.Sep 30, 2018 · N372NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018093005880Stop Fitting · crackedCRACK INDICATION ON FRAME 16 IN OPEN HOLE INBOARD UPPER POSITION DOOR STOP FITTING NR 7 LEFT HAND SIDE AT FORWARD GALLEY AREA. REPLACED INTERCOSTAL FITTING IAW SRM 51-42-11 AND 51-72-11 AND DWG D53112319.Sep 29, 2018 · N372NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2018092905843Floorbeam · corrodedCORROSION FLOORBEAM +Y1292 LOCATED FROM FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D5311084.Sep 28, 2018 · N372NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018092905842Floorbeam · corrodedCORROSION FLOORBEAM +Y1162.5 FRAME 68 TO FRAME 69 AT AFT GALLEY AREA. REPLACED IAW SRM 51-72-11 AND DWG D53472001.Sep 28, 2018 · N372NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018100105806Floorbeam · corroded(LP# 0760437) CORROSION FLOOR BEAM -Y765 FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA (SSI 531189) REPLACED IAW SRM 51-72-11,51-42-11 AND DWG D53110984.Sep 27, 2018 · N372NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018100105804Crossbeam · damaged(LP# 0760471) ELONGATED HOLE CROSSBEAM AT LEVEL STRINGER 23R AND FRAME 67 AND -Y162.5 AT AFT GALLEY AREA. REPLACED IAW SRM 51-42-11 AND DWG 53474250.Sep 27, 2018 · N372NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018100105803Floorbeam · corroded(LP# 0760455) CORROSION FLOOR BEAM =Y1292 FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA (SSI 531189). REPLACED IAW SRM 51-72-11 AND DWG D53110830.Sep 27, 2018 · N372NW · Airbus A320212 · Fuselage Main, Floor BeamSDR DALA2018100105802Shear Tie · corroded(LP# 0760427) CORROSION SHEAR TIE AT LEVEL FRAME 30 BETWEEN STRINGER 41R TO STRINGER 42R IN FORWARD CARGO COMPARTMENT. REPLACED IAW SRM 51-72-11 AND DWG D53231586.Sep 27, 2018 · N372NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2018100105801Shear Tie · corroded(LP# 0760413) CORROSION SHEAR TIE AT FRAME BETWEEN STRINGER 42L TO STRINGER 43L IN FORWARD CARGO COMPARTMENT. REPLACED IAW SRM 51-72-11 AND DWG D53230319.Sep 27, 2018 · N372NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2018100105800Shear Tie · corroded(LP# 0760394) CORROSION SHEAR TIE LOCATED AT FRAME 28 BETWEEN STRINGER 42R TO STRINGER 42R IN FORWARD CARGO COMPARTMENT. REPLACED IAW SRM 51-72-11 AND DWG D53231586.Sep 27, 2018 · N372NW · Airbus A320212 · Fuselage Internal Mounting StructureSDR DALA2018100105799Web · corroded(LP# 0760374) CORROSION FLOOR STRUCTURE WEB LOCATED BETWEEN FRAME 65 TO FRAME 66 AND STRINGER 23R AT AFT GALLEY AREA. REPLACED IAW SRM 51-42-11 AND DWG D53474250.Sep 27, 2018 · N372NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018092705780Floor Support · corroded(LP# 0758763) CORROSION FLOOR BEAM -Y254 FRAME 12 TO FRAME 24 AT FORWARD GALLEY AREA (SSI 531189). REPLACED FLOOR BEAM IAW SRM 51-72-11 AND DWG D53110920.Sep 26, 2018 · N372NW · Airbus A320212 · Fuselage Miscellaneous StructureSDR DALA2018092705779Crossbeam · damaged(LP# 0758747) ELONGATED HOLE CROSSBEAM SECTION LOCATED FR68 AT LEVEL STF23LAT AFT GALLEY AREA. REPLACED CROSSBEAM SECTION IAW SRM 51-72-11 AND DWG D53474250 ISSUE V.Sep 26, 2018 · N372NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2017013000811Wire · out of positionEMERGENCY EXIT SIGNS INOPERATIVE DOOR 2R, FOUND WIRE MISCONNECTED, REINSTALLED CORRECTLY.Jan 28, 2017 · N372NW · Airbus A320212 · Light System WiringSDR DALA2017010400180Fitting · corrodedCORROSION ON THE FWD FITTING FIXED BUSHING FOR THE KEEL BEAM IN THE LT MLG DOOR IN MAIN WHEEL WELL, REPLACED THE FITTING IAW SRM 51-72-11 AND DRAWING D53370600.Jan 3, 2017 · N372NW · Airbus A320212 · Fuselage, Landing Gear Attach FittingsSDR DALA2017010300179Box Beam · crackedCRACK INDICATION FOUND ON THE SIDE BOX BEAM. REPAIRED IAW AMDS CARD 5310-01450-02.Dec 30, 2016 · N372NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2017010300178Box Beam · crackedCRACK INDICATION FOUND ON THE SIDE BOX BEAM AT FRAME 43. REPAIRED IAW AMDS 5310-01450-02.Dec 30, 2016 · N372NW · Airbus A320212 · Fuselage Main, StructureSDR DALA2016122810167Skin · dentedDENT ON L/E EXTERNAL SKIN O/B SIDE END ON SLAT 3 ON RT WING, PERMANENT REPAIR ON LEADING EDGE OF EXTERNAL SKIN OUTBOARD SIDE END ON SLAT 3 ON RH WING AS PER SRM 57-44-21 PAR. 5E(3) FIG. 206 (SHEET 4)Dec 27, 2016 · N372NW · Airbus A320212 · Leading Edge DevicesSDR DALA2016020600955Stringer · corrodedSTRINGER S42L BETWEEN FRAMES 56-57 HAS EVIDENCE OF CORROSION . REMOVED CORROSION IAW SRM 51-74-00. REPAIRED THE STRINGER IAW SRM 53-00-13, FIG 201, SRI 53-00-13-2-001-00.Feb 5, 2016 · N372NW · Airbus A320212 · Fuselage Main, Longeron/StringerSDR DALA2016020600954Stringer · corrodedTHERE IS EVIDENCE OF CORROSION ON S42L BETWEEN FRAMES 56 & 57, REMOVED CORROSION IAW SRM CH 51-74-00, REMAINING MATERIAL IS .095, REPAIR STRINGER 43L IAW SRM 53-00-13 FIG 201, SRI 53-00-13-2-001-00.Feb 5, 2016 · N372NW · Airbus A320212 · Fuselage Main, Longeron/Stringer
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